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Wind tunnel investigation of the flow field under a 60 degree swept wing at Mach numbers from 0.6 to 2.6Wind tunnel studies of flow field under 60 deg swept wing from Mach 0.6 to 2.6
Document ID
19690013457
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Blaha, B. J. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
April 1, 1969
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-52585
Accession Number
69N22822
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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